North American T-6 Texan vs. Northrop T-38 Talon

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North American T-6 Texan versus Northrop T-38 Talon
9.0 m 29 ft 6 in length 14.1 m 46 ft 4 in
3.56 m 11 ft 8 in height 3.9 m 12 ft 10 in
12.8 m 42 ft wingspan 7.7 m 25 ft 3 in
1 x Pratt & Whitney R-1340-AN-1 radial engine engines Two General Electric J85-GE-5A turbojet engines
Approximately 600 hp thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Approximately 600 hp total thrust 4,100 pounds dry thrust; 5,800 with afterburners
5,617 lb 2,548 kg MTOW 12,093 lb 5,485 kg
1,175 km 634 nm range 1,759 km 950 nm
145 mph 233 km/h cruise speed 745 kts 1,380 km/h
Pilot and one passenger capacity Two (student and instructor)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.